# STC SH5200NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Air Methods Corporation, United States
- Description: Installation of main rotor electrostatic bonding straps.
- Applied: November 16, 1990
- Status date: March 8, 1995
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW)
- Certificate PDF: https://openairdocs.org/files/sha256/c3/c5/c3c501447501715f19968f9729ff7803618104a848970008f56cc9dcd1668d78
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C508B629C79E6EBA85256CC2005C32D7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SH5200NM

## ADs that name it (0)

None.

## Approved models (3)

- Bell Helicopter Textron Inc. 412 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW))
- Bell Helicopter Textron Inc. 412CF ([TCDS H4SW](https://openairdocs.org/tcds/H4SW))
- Bell Helicopter Textron Inc. 412EP ([TCDS H4SW](https://openairdocs.org/tcds/H4SW))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SH5200NM This certificate issued to: Air Methods Corporation Part 29 of the Federal Aviation Regulations.

Original Product -Type Certificate Number: H4SW Make: Bell Helicopter Textron Model: 412, 412EP (S/N: 36087 & Subsequent), 412CF (S/N: 46400 & Subsequent) Description of Type Design Change:

Installation of main rotor electrostatic bonding straps in accordance with Air Methods Corporation Master Drawing List No. 141-9006, revision N/C, FAA approved December 7, 1990, or later approved revision.

Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft.

Date of Application: November 16, 1990 Date Reissued:

Date of Issuance: December 7, 1990 Date Amended: March 8, 1995 FEDERAL AVIATION By Direction of the Administrator ROMAN T. GABRYS (Signature) Actiog Manager OMINIST RATION Denver Aircraft Certification Office Northwest Mountain Region, Denver, Colorado (Title)

## Every issue (1)

- March 8, 1995: Amended, Current. [certificate](https://openairdocs.org/files/sha256/c3/c5/c3c501447501715f19968f9729ff7803618104a848970008f56cc9dcd1668d78)

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